GB1424292A - Load carrying and ejecting device - Google Patents
Load carrying and ejecting deviceInfo
- Publication number
- GB1424292A GB1424292A GB1150874A GB1150874A GB1424292A GB 1424292 A GB1424292 A GB 1424292A GB 1150874 A GB1150874 A GB 1150874A GB 1150874 A GB1150874 A GB 1150874A GB 1424292 A GB1424292 A GB 1424292A
- Authority
- GB
- United Kingdom
- Prior art keywords
- load
- core
- sleeve
- coupling means
- piston
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 230000008878 coupling Effects 0.000 abstract 4
- 238000010168 coupling process Methods 0.000 abstract 4
- 238000005859 coupling reaction Methods 0.000 abstract 4
- 230000000712 assembly Effects 0.000 abstract 1
- 238000000429 assembly Methods 0.000 abstract 1
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 238000006073 displacement reaction Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bombs doors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Control Devices (AREA)
- Toys (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
1424292 Supporting and ejecting device RAFAUT & CIE 14 March 1974 [27 March 1973] 11508/74 Heading F3C A device for supporting on and ejecting a load C from an aircraft comprises two assemblies A, B each intended to co-operate with a different bore in the load C, each assembly comprising a sleeve 2 carrying a detent or wedge coupling means. The detent or wedge coupling means is actuated for supporting the load by displacement of a core 8 within the sleeve 2 and a linkage 15, (18) connects the core 8 to a common lock-unlock control 19. Lifting means are provided for urging the sleeve 2 and, in use, its associated load upwardly and also ejection pistons 31, 31<SP>1</SP> for urging, in use, the load away from the device. Gas under pressure is used for actuation of the common lock-unlock control 19 and the ejection pistons. As shown the actuator for the common lockunlock control 19 comprises a piston 23 which is held against actuation by a removable pin 32. Pressurized gas is produced by a cartridge fired in a chamber 26, the gas first actuating the piston 23, the pin 32 having been removed, and the piston 23 after its actuating travel opening channels 28, 28<SP>1</SP> leading to the ejection pistons 31, 31<SP>1</SP>. The detent coupling means comprise balls 5 which are urged into their active position by a large diameter portion 9 of the core 8, the core 8 being urged to its coupling means actuating condition by a spring loaded member 8a being urged upwardly by the load C being brought to the device. The sleeve lifting means comprises a manually operable rack 6, 7. The linkages are also manually operable through a formation 20.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7310960A FR2223236B1 (en) | 1973-03-27 | 1973-03-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1424292A true GB1424292A (en) | 1976-02-11 |
Family
ID=9116922
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1150874A Expired GB1424292A (en) | 1973-03-27 | 1974-03-14 | Load carrying and ejecting device |
Country Status (5)
Country | Link |
---|---|
US (1) | US3883097A (en) |
BE (1) | BE812154A (en) |
DE (1) | DE2414631A1 (en) |
FR (1) | FR2223236B1 (en) |
GB (1) | GB1424292A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4203173B4 (en) * | 1991-02-18 | 2005-05-12 | Volkswagen Ag | Internal shoe drum brake for motor vehicles |
CN109625270A (en) * | 2018-12-29 | 2019-04-16 | 中航电测仪器股份有限公司 | A kind of helicopter handling carry device and its operation method |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2316652A1 (en) * | 1975-07-02 | 1977-01-28 | Alkan R & Cie | PRESSURE CONTROLLER FOR AIRPLANE LOAD PYROTECHNICAL EJECTOR |
US3974990A (en) * | 1975-07-21 | 1976-08-17 | The United States Of America As Represented By The Secretary Of The Navy | Dual ejector stores attitude control system |
US4015507A (en) * | 1976-03-25 | 1977-04-05 | The United States Of America As Represented By The Secretary Of The Navy | Ejection system |
US4187759A (en) * | 1977-09-16 | 1980-02-12 | The United States Of America As Represented By The Secretary Of The Navy | Separation nut system |
US4181062A (en) * | 1978-07-10 | 1980-01-01 | The United States Of America As Represented By The Secretary Of The Navy | Release assembly using separation nuts and thrusters |
US4257639A (en) * | 1979-12-17 | 1981-03-24 | Rockwell International Corporation | Ejector device for stores |
US4388853A (en) * | 1980-07-24 | 1983-06-21 | Frazer-Nash Limited | Missile launchers |
US4448373A (en) * | 1980-12-15 | 1984-05-15 | The United States Of America As Represented By The Secretary Of The Navy | Elastomeric sway bracing and ejector system |
EP0070275B1 (en) * | 1981-01-26 | 1987-11-04 | Rockwell International Corporation | An ejector device for stores |
US4441674A (en) * | 1981-02-05 | 1984-04-10 | The United States Of America As Represented By The Secretary Of The Navy | Constrained store ejector |
DE3227628A1 (en) * | 1981-07-22 | 1986-11-13 | Frazer-Nash Ltd., Kingston-upon-Thames, Surrey | AIRPLANE EJECTOR RELEASE UNIT |
US4523731A (en) * | 1983-09-28 | 1985-06-18 | The Boeing Company | External store release for flight vehicle |
US4606517A (en) * | 1983-12-12 | 1986-08-19 | Northrop Corporation | Store adapter |
FR2573383B1 (en) * | 1984-11-16 | 1987-02-06 | Dassault Avions | DEVICE FOR EJECTING A LOAD HANGED UNDER A HIGH PERFORMANCE AIRCRAFT |
US4674407A (en) * | 1986-06-02 | 1987-06-23 | The United States Of America As Represented By The Secretary Of The Navy | Lug assembly for bomb to bombrack attachment |
FR2720371B1 (en) * | 1994-05-31 | 1996-08-23 | Aerospatiale | Mechanical ejection device comprising a movable piston controlled in return. |
US5406876A (en) * | 1994-06-21 | 1995-04-18 | Northrop Grumman Corporation | Store retention and release system |
US6009788A (en) * | 1997-12-10 | 2000-01-04 | Mcdonnell Douglas Corporation | Variable flow-restricting device and method |
US8869671B2 (en) * | 2012-08-14 | 2014-10-28 | Raytheon Company | Aircraft device deployment system with spring-driven mechanical linkage |
KR101873067B1 (en) * | 2012-11-20 | 2018-06-29 | 국방과학연구소 | Weapn station |
US9783296B2 (en) | 2014-09-18 | 2017-10-10 | Raytheon Company | Aircraft store deployment system with improved safety of arming and releasing stores |
KR101701975B1 (en) | 2016-04-08 | 2017-02-13 | 유효선 | Vertical free falling apparatus for dropping objects airdrop |
US10414488B2 (en) * | 2016-09-09 | 2019-09-17 | Wing Aviation Llc | Methods and systems for damping oscillations of a payload |
CN107097956B (en) * | 2017-05-27 | 2023-09-01 | 南京理工大学 | Multifunctional bullet picking device equipped in unmanned aerial vehicle |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2822207A (en) * | 1953-11-20 | 1958-02-04 | North American Aviation Inc | Release ejector |
US3557550A (en) * | 1968-02-05 | 1971-01-26 | Whittaker Corp | Pressure-controlled bomb ejector for aircraft |
GB1248926A (en) * | 1968-08-08 | 1971-10-06 | Ml Aviation Co Ltd | Ejector release units for use in aircraft |
-
1973
- 1973-03-27 FR FR7310960A patent/FR2223236B1/fr not_active Expired
- 1973-12-10 US US423351A patent/US3883097A/en not_active Expired - Lifetime
-
1974
- 1974-03-11 BE BE141891A patent/BE812154A/en not_active IP Right Cessation
- 1974-03-14 GB GB1150874A patent/GB1424292A/en not_active Expired
- 1974-03-26 DE DE2414631A patent/DE2414631A1/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4203173B4 (en) * | 1991-02-18 | 2005-05-12 | Volkswagen Ag | Internal shoe drum brake for motor vehicles |
CN109625270A (en) * | 2018-12-29 | 2019-04-16 | 中航电测仪器股份有限公司 | A kind of helicopter handling carry device and its operation method |
Also Published As
Publication number | Publication date |
---|---|
US3883097A (en) | 1975-05-13 |
FR2223236A1 (en) | 1974-10-25 |
BE812154A (en) | 1974-07-01 |
FR2223236B1 (en) | 1975-08-22 |
DE2414631A1 (en) | 1974-10-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |